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On the use of Euler's theorem on rotations for the synthesis of attitude control systemsEuler theorem applied to rotations for synthesis of attitude control systems
Document ID
19660027747
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Meyer, G. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
September 1, 1966
Subject Category
Space Sciences
Report/Patent Number
NASA-TN-D-3643
Report Number: NASA-TN-D-3643
Accession Number
66N37037
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
ATTITUDE CONTROL
ROTATION
EULER EQUATION

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